EP2567382B1

EP2567382B1 - Localised energy concentration

Info

Publication number: EP2567382B1
Application number: EP11721572.3A
Authority: EP
Inventors: Yiannis Ventikos; Nicholas Hawker
Original assignee: Oxford University Innovation Ltd
Current assignee: Oxford University Innovation Ltd
Priority date: 2010-05-07
Filing date: 2011-05-09
Publication date: 2016-08-31
Anticipated expiration: 2031-05-09
Also published as: US10315180B2; CA2798586C; RU2012149609A; JP2015222256A; BR112012028461A2; ES2600679T3; KR101772525B1; US9530524B2; CN102884586B; US20130114774A1; MX2012012898A; RU2547829C2; AU2011249596A1; AU2011249596B2; EP3101655A1; CA2798586A1; ZA201208197B; JP6040287B2; EP2567382A1; EP3101656A1

Description

This invention relates to methods and apparatuses for producing very high localised energies. It relates particularly, although not exclusively, to generating localised energies high enough to cause nuclear fusion.
The development of fusion power has been an area of massive investment of time and money for many years. This investment has been largely centred on developing a large scale fusion reactor, at great cost. However, there are other theories that predict much simpler and cheaper mechanisms for creating fusion. Of interest here is the umbrella concept "inertial confinement fusion", which uses mechanical forces (such as shock waves) to concentrate and focus energy into very small areas.
Much of the confidence in the potential in alternative methods of inertial confinement fusion comes from observations of a phenomenon called sonoluminescence. This occurs when a liquid containing appropriately sized bubbles is driven with a particular frequency of ultrasound. The pressure wave causes bubbles to expand and then collapse very violently; a process usually referred to as inertial cavitation. The rapid collapse of the bubble leads to non-equilibrium compression that causes the contents to heat up to an extent that they emit light [Gaitan, D. F., Crum, L. A., Church, C. C., and Roy, R. A., Journal of the Acoustical Society of America, 91(6), 3166-3183 June (1992)]. There have been various efforts to intensify this process and one group has claimed to observe fusion [Taleyarkhan, R. P., West, C. D., Cho, J. S., Lahey, R. T., Nigmatulin, R. I., and Block, R. C., Science, 295(5561), 1868-1873 March (2002)]. However, the observed results have not yet been validated or replicated, in spite substantial effort [Shapira, D. and Saltmarsh, M., Physical Review Letters, 89(10), 104302 September (2002)]. This is not the only proposed mechanism that has led to luminescence from a collapsing bubble; however it is the most documented. Luminescence has also been observed from a bubble collapsed by a strong shock wave [Bourne, N. K. and Field, J. E., Philosophical Transactions of the Royal Society of London Series A-Mathematical Physical and Engineering Sciences, 357(1751), 295-311 February (1999)]. It is this second mechanism, i.e. the collapse of a bubble using a shockwave, to which this invention relates. It has been proposed in US 7445319 to fire spherical drops of water moving at very high speed (∼1 km/s) into a rigid target to generate an intense shock wave. This shock wave can be used to collapse bubbles that have been nucleated and subsequently have expanded inside the droplet. It is inside the collapsed bubble that the above-mentioned patent expects fusion to take place. The mechanism of shockwave generation by high-speed droplet impact on a surface has been studied experimentally and numerically before and is well-documented (including work by one of the present patent inventors, [Haller, K. K., Ventikos, Y., Poulikakos, D., and Monkewitz, P., Journal of Applied Physics, 92(5), 2821-2828 September (2002)].) The present invention differs from US 7445319 , even though the fundamental physical mechanisms are similar, because it does not utilise a high speed droplet impact.
The present invention aims to provide alternatives to the aforementioned techniques and may also have other applications. When viewed from a first aspect the invention provides a method of producing a localised concentration of energy as claimed in claim 1.
The invention also extends to an apparatus for producing a localised concentration of energy as claimed in claim 15.
It is known to those skilled in the art that in general an interaction between a shockwave in a non-gaseous medium and a gas bubble in that medium can generate a high speed transverse jet of the non-gaseous medium that moves across the bubble, impacting the leeward bubble wall. This is one of the mechanisms which gives rise to the well-known problem of cavitation damage of surfaces when shockwaves are generated in the presence of micro-bubbles formed on the surface. In accordance with the present invention however, the inventors have appreciated that this naturally-occurring phenomenon can be appropriately adapted and harnessed to produce very high localised energy concentration which can be used, e.g. to create nuclear fusion as will be explained later.
The phenomenon of a jet being formed during bubble collapse is controlled to promote formation of this transverse jet and enhancement of its speed, and the surface depression is designed to receive the transverse jet impact whilst trapping a small volume of the original gas pocket between the impacting jet and itself. This leads to various physical mechanisms that cause very substantial energy focusing in this volume of trapped gas.
More particularly by designing the depression in the surface explicitly to receive the high speed jetting formed by the interaction of the incident shockwave with the gas pocket, then as the incident shock interacts with the surface of the gas pocket, it forms a transmitted shock and a reflected rarefaction. If the contact is the correct shape, i.e. curving away from the incident shockwave, then this rarefaction will act to focus the flow to a point. This then results in the formation of the high speed transverse jet which can, purely as an example, reach over 2000ms^-1 for a 1 GPa shockwave. When this jet strikes the surface of the depression a strong shockwave is generated within by the force of the impact in a manner analogous to the high speed droplet impact situation described in US 7445319 .
The shape of the surface in the depression opposite where the shockwave is incident could be flat so that the jet contacts the surface at a point. In a preferred set of embodiments however the surface depression and gas pocket are arranged such that the initial contact region is a curve which forms a closed loop - e.g. a ring. This makes it possible to trap a portion of the gas pocket between the jet tip and the edge of the depression. To achieve this, a section of the target surface has a curvature greater than that of the tip of the jet and this part of the surface is placed such that the jet impacts into it. Upon impacting, a toroidal shockwave is generated whose inner edge propagates towards the base of the depression and towards the trapped portion of gas. Combining this with the 'piston' effect of the gas halting the motion of the impacting jet yields extremely strong heating of the trapped gas. For example, for a given strength of shockwave the peak temperatures can be increased by over an order of magnitude by these arrangements as compared to a bubble attached to a planar surface.
The depression could take a number of shapes. In a set of embodiments it tapers in cross-section away from the mouth. The depression could resemble a dish - e.g. being continuously curved. The surface need not be continuously curved however. In a set of embodiments the surface more closely resembles a crack rather than a dish shape. This could be defined by stating that the depth is greater than the width or by the presence of a region of curvature at the tip of the crack greater than the curvature (or maximum curvature) of the portion of the gas pocket received in it. In one set of embodiments the surface comprises a plurality of discrete portions, e.g. with a gradient discontinuity between them. The portions could themselves be partial ellipses, parabolas, and so on, but equally could be straight. A particular set of embodiments of surfaces made from discrete portions could be described as piecewise polynomial.
As above, the bubble could be small in comparison to the dimensions of the crack such that it is attached only to one side or it could be of similar size so as to close it off. It is not essential that there is only one depression which partly receives the gas pocket; a gas pocket could extend across, and be partially received by, a plurality of depressions.
In a particular set of embodiments the high speed jet is arranged to strike an area of surface that has been prepared with a particular roughness or microscopic shape such that many small portions of the pocket of gas are trapped between the jet tip and the target surface, i.e. the many small depressions are small in comparison to the size of the transverse jet tip.
As before, there are many shapes and configurations which the surface might take to provide suitable regions for attaching the pocket of gas to the surface and the configuration of the surface will determine how the shockwave interacts with it and the shape of the surface relative to the placement and shape of the bubble will determine how the shockwave interacts with the gas pocket, which it may do so before, simultaneously or after it interacts with the surface. This in turn affects the dynamics of the collapse and hence can increase temperatures and densities that are achievable through compression of the gas by the shockwave. In some embodiments, the peak temperatures can be increased by over an order of magnitude, when compared with a similar shock interacting with an isolated bubble.
In a preferred set of embodiments, the surface is concave which has the effect of focussing the energy and intensifying the initial formation of the shockwave. In some non-limiting examples, the surface could have an ellipsoid or paraboloid shape. The surface need not be continuously curved. For example, in one set of embodiments the concave surface comprises a plurality of discrete portions, e.g. with a gradient discontinuity between them. The portions could themselves be partial ellipses, parabolas, and so on, but equally could be straight. A particular set of embodiments of surfaces made from discrete portions could be described as piecewise polynomial. The gas pocket could be attached to any part of the surface but is preferably attached to the bottom or centre point.
The dimensions of the gas pocket could be small in comparison to the width or depth of the concave surface - e.g. so as to be attached only to one side of the concavity, or it could of similar size - e.g. so as to attach to the surface in an annulus around the base of the depression.
The concavity could resemble a bowl - e.g. being continuously curved. In a set of embodiments however the surface more closely resembles a crack rather than a bowl shape. This could be defined by stating that the depth is greater than the width or by the presence of a region of curvature at the tip of the crack greater than the curvature (or maximum curvature) of the bubble. As above, the gas pocket could be small in comparison to the dimensions of the crack such that it is attached only to one side or it could be of similar size so as to close it off.
In one set of embodiments the shape of the surface is configured to trigger a transition from regular to Mach reflection of the incident shockwave, thus altering the shape of the shockwave that then reaches the gas pocket. In another set of embodiments the shape is controlled such that the reflections overlap and interact with one another, again acting to change the shape of the shockwave or interacting system of shockwaves when it contacts the gas pocket. By carefully controlling these factors an intensification of the peak temperatures can be obtained over the case where the surface is planar.
In a particular set of embodiments the surface might have a plurality of concave portions. Additionally or alternatively the or each concave portion may have a plurality of gas pockets attached thereto.
The surface comprises a depression shaped so as partially to receive the gas pocket, thereby exploiting the jetting phenomenon and away from the depression the surface could be shaped to concentrate the intensity of the shockwave which is incident upon the pocket of gas. This could allow the properties of the jet - e.g. its speed - to be controlled to maximise the concentration of energy. Such combinations could be beneficial in providing the desired behaviour of the shockwave within the depression in other ways.
The bubble is attached to the surface and this could be over a single contact patch or, by appropriate design of the surface texture, at a plurality of discrete contact points/regions.
As well as creating a particular shape for the target surface, in one set of embodiments the micro-structure or wetting characteristics of the surface can be optimised to control the speed of the shockwave near the surface, e.g. to increase the speed near the surface, thereby changing the shockwave's shape and hence the nature of the interaction between the shockwave and the gas pocket. As previously discussed, an appropriately shaped gas pocket can be used in this set of embodiments to match the shape of the shockwave to the shape of the gas pocket, thereby allowing the dynamics of the gas pocket's collapse to be controlled in order to maximise the temperature and density achieved on compression.
The surface to which the gas pocket is attached is not limited to having a single depression (e.g. to exploit the jetting phenomenon described above) and thus in one set of embodiments, the target surface comprises a plurality of depressions. Each individual depression may be shaped to encourage energy focusing by causing the shockwave to converge on one or more bubbles. That is to say, the surface may be prepared with more than one site where the shockwave will interact with a shaped section of surface containing either an attached or nearby gas pocket, thus providing infinite scalability. An advantage of employing a plurality of depressions is that a greater proportion of the shockwave energy may be harnessed. For example, a large pocket of gas could be spread across a plurality of depressions, or smaller individual volumes of gas could be located within each individual depression. For the former case, depending upon the number of such depressions, the size of an individual depression will be significantly smaller than the size of the pocket of gas. For a larger volume of medium able to accommodate a large number of depressions, this points towards simplicity of manufacturing for an energy-producing fusion apparatus.
Such pluralities of depressions could be formed in a number of ways. For example, a solid surface could be drilled or otherwise machined to produce depressions or pits. In one set of embodiments, however, the depressions are created by the surface texture of the surface. For example, the surface could be blasted with an abrasive material, etched or otherwise treated to give a desired degree of surface roughness which provides, at the microscopic level, a large number of pits or depressions.
The surface could be constructed from a solid, as implied in many of the embodiments outlined above, but it could equally well be a liquid. In the case of a solid, any of the proposed materials in US 7445319 could be suitable. In the case of a liquid the required surface shape could be achieved in a number of ways. For example, the surface of a volume of liquid could be excited with a suitable vibration (e.g. using ultrasound or another method) to generate a wave having the desired shape. Alternatively the desired shape could be achieved through the contact angle between a liquid and a solid surface with appropriately matched wetting properties. Of course, this latter example shows that the surface could comprise a combination of solid and liquid. Where the target surface comprises a liquid it will generally be denser than the non-gaseous medium.
Of course, as has already been alluded to, some embodiments may comprise a plurality of pockets of gas within the medium. These pockets of gas may all be attached to the surface or some may be positioned near the target surface.
The aspects of the invention described herein provide alternatives to the technique described in US 7445319 which may carry their own benefits. The present inventors have recognised that there are significant challenges in the nucleation of a bubble in a droplet fired at high speed into a target, as suggested in US 7445319 . The timing will have to be very precise for the bubble to be at a favourable moment of its expand-collapse cycle when the shock strikes. The method by which the high speed droplets are created as required by US 7445319 and detailed in US 7380918 is also complex and expensive. By contrast such complexity and associated expense can be avoided in accordance with at least preferred embodiments of the present invention. Thus, the invention provides much simpler techniques for compressing a volume of gas entrapped in a gas pocket as a shockwave simply needs to be created within the medium in which the gas pocket is formed. Moreover the theoretical and computer modelling of both techniques carried out by the present inventors suggests that the method in accordance with the present invention can give pressure and temperature intensities which are an order of magnitude greater than the method detailed in US 7445319 .
The more static framework that can be employed in accordance with the invention to compress a gas pocket using a shockwave allows much greater control (compared to a free bubble) over how the shockwave strikes and interacts with the pocket.
The initial shockwave could be created in a number of different ways by a number of different devices depending on the pressure required. For example, a shockwave lithotripsy device could be used to generate lower intensity shockwaves or an explosive plane wave generator could be used to provide high intensity shockwaves. In preferred embodiments such an explosive device can create a shockwave pressure of between 0.1 GPa and 50 GPa, and in another preferred embodiment a lithotripsy device could be used to generate shockwave pressures of 100 MPa to 1 GPa.
The term "gas" as used herein should be understood generically and thus not as limited to pure atomic or molecular gases but also to include vapours, suspensions or micro-suspensions of liquids or solids in a gas or any mixture of these. The "non-gaseous medium" should be understood generically and thus could include liquids, non-Newtonian liquids, semi-solid gels, materials that are ostensibly solid until the passage of the shockwave changes their properties, suspensions or micro-suspensions and colloids. Examples include but are not limited to water, oils, solvents such as acetone, hydrogels and organogels. It should be understood that the liquid will have a greater density than the gas in the pocket.
The non-gaseous medium could be any suitable substance for creating a shockwave in, such as a liquid or a semi-solid gel. The gas pocket can then be provided by a bubble suspended within the liquid or gel medium in the required location attached to the target surface. Using a gel or a viscous liquid has the advantage that it is easier to control the location of the bubble within the medium, compared to a lower viscosity liquid in which the buoyancy of the bubble may overcome the viscosity of the liquid. The bubble is attached to the target surface, the nature of the target surface, e.g. the material, or any indentations or depressions in it, could help to adhere the bubble to the target surface. Using a gel or viscous liquid also has the advantage that it will be easier to control the detailed shape of the bubble.
Due to the more static nature of the setup of the device when compared to US 7445319 , much more control can be exercised over the shape of the bubble. The bubble may be spherical in shape apart from where it is truncated by its attachment to the target surface, for example it could be hemi-spherical. In some embodiments the bubble joins the target surface normal to it whereas in others a different angle is required. In a superset of these embodiments the bubble itself is not spherical in nature but takes a different shape that includes but is not limited to ellipsoids, cardioids, variations from spherical, cardioid or ellipsoid shape in which the surface has perturbations that could be described, for example, by a Fourier series and bubbles with other distinct shapes such as cones or trapezoids. It will be apparent that, for example, a conical bubble would be difficult to achieve in a true liquid medium but that in the case of a gel medium this set of embodiments becomes possible and could be advantageous.
The gas pocket itself must be formed in some manner. In a particular set of embodiments it is nucleated using a system similar to that described in US 7445319 , where a laser is used in conjunction with nano-particles in the liquid to nucleate a bubble. In a different set of embodiments a bubble could be nucleated using an unstable emulsion of different liquids. In another set the bubble is nucleated using an appropriately targeted pressure wave designed to induce cavitation in the liquid. As the gas pocket is attached to the wall, a specifically controlled volume of gas could be pumped in through a passage in the target surface in order to expand a bubble on the surface. This set of embodiments has the advantage of great control over the contents and size of the gas pocket generated. In the set of embodiments where the liquid medium is a gel the gas pocket can be pre-manufactured by punching or otherwise cutting out or moulding the correct shape from the gel block to be used.
In another set of embodiments the gas pocket is formed with the use of a pre-manufactured membrane that defines the boundary between the gas pocket and the medium and hence also defines the gas pocket's shape. The use of a thin membrane in this manner allows a decoupling of the liquid and gas materials, allowing any choice of combination of compositions to be made. It also allows the shape of the gas pocket to be controlled with a precision not available to other methods. The membrane could be formed from any suitable material, e.g. glass e.g. plastic e.g. rubber. Having a prefabricated membrane allows a liquid medium to be used more easily as the volume of gas is trapped against the target surface and therefore cannot float away or be otherwise disturbed. In a particular set of embodiments the membrane is frangible and is arranged to break upon impact from the shockwave such that it has no influence on the resulting dynamics. In one set of embodiments the prefabricated membrane includes a line or region of weakness, so that upon impact from the shockwave it breaks along the line or in the region of weakness. The line or region of weakness can be arranged so that the position of the breach has an influence on the ensuing flow patterns, for example this could help control the formation and dynamics of the transverse jetting. In another set of embodiments the membrane is designed to deform with the collapsing cavity.
In a preferred set of embodiments, the methods described herein are employed to generate nuclear fusion reactions. The fuel for the reaction could be provided by the gas in the pocket, the medium, or the fuel could be provided by the target surface itself. Any of the fuels mentioned in US 7445319 is suitable for use in the present invention.
The device in the present invention is not as restricted, regarding size, as US 7445319 where the size of the droplet constrains the maximum bubble size. It may be advantageous to have a larger apparatus where a larger volume of gas is heated. The volume of gas in each pocket may be chosen depending on the circumstances but in one set of preferred embodiments it is between 5 x 10^-11 and 5 x 10^-3 litres.
The fusion reactions which can be obtained in accordance with certain embodiments of the invention could be used for net energy production (the long term research aim in this field), but the inventors have appreciated that even if the efficiency of the fusion is below that required for net energy production, the reliable fusion which is obtainable in accordance with embodiments of the invention is advantageous for example in the production of tritium which can be used as fuel in other fusion projects and is very expensive to produce using currently existing technologies. The fusion can also be beneficial in giving a fast and safe neutron source which has many possible applications that will be apparent to those skilled in the art.
Moreover, it is not essential in accordance with the invention to produce fusion at all. For example, in some embodiments the techniques and apparatus of the present invention may be advantageously employed as a sonochemistry reactor which can be used to access extreme and unusual conditions.
Certain embodiments of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:

Figs. 1 a and 1 b show two variants of a target surface in accordance with one aspect of the invention;
Figs. 2a and 2b show two successive stages of an interaction of a shockwave with a pocket of gas in accordance with another aspect of the invention;
Fig. 3 shows a further embodiment of the invention; and
Fig. 4 shows a variant of the embodiment of Fig. 2a.

Figs. 1 a and 1 b show schematically arrangements in accordance with two respective embodiments of one aspect of the invention. In each case a solid surface 6, for example made from high strength steel, is placed inside a non-gaseous medium 8 in the form of a hydrogel, for example a mixture of water and gelatine. Defined in the hydrogel medium 8 is a gas pocket 2 filled with vaporous fuel suitable for taking part in a nuclear fusion reaction. In both cases the gas pocket 2 is attached to the target surface 6 inside a concave depression. In the case of the first embodiment in Fig. 1 a, the depression 4 is parabolic and relatively large such that only one side of the gas pocket 2 is attached to the surface 6. The size of the apparatus is flexible but a typical dimension of this diagram could be between 0.1 and 1x10^-5 m.
In the case of the second embodiment in Fig. 1 b, the gas pocket 2 is received in a much smaller, V-shaped tapering depression 5 which could be machined or formed as the result of a naturally occurring crack in the surface 6.
In operation a shockwave 10 is created from an explosion, for instance with a pressure of 5 GPa, within the gel medium 8. This is represented in both Figs. 1 a and 1 b as a line propagating in the direction of the arrow towards the pocket of gas 2. First the shockwave 10 strikes the upper parts of the target surface 6, causing the shockwave 10 to change shape as it advances towards the pocket of gas 2. In this manner the shape of the shockwave 10 that advances into the pocket of gas 2 can be explicitly controlled by shaping the surface 6 accordingly. The shaped shockwave 10 will then strike the pocket of gas 2, compressing it against the target surface 6 as the shockwave 10 propagates through the gas pocket 2. Reflections of the shockwave 10 from the surface 6 after it has propagated through the pocket 2 travel back through the pocket, reinforcing those propagating from the original direction and further compressing the gas pocket. The compression of the gaseous fuel inside the pocket causes intense local heating which can be sufficient to generate a nuclear fusion reaction.
Figs. 2a and 2b show, in accordance with yet another aspect of the invention, two successive stages of a shockwave interaction with a pocket of gas 22 attached to a surface 26 so as to cover and fill a V-shaped tapering depression 24. Although the tapering depression 24 is of a similar shape to that in Fig. 1 b, relative to the size of the tapering depression, the volume of gas in the pocket 22 is much greater than it is in Fig. 1 b. For example the width of the bubble could be of the order of 1 cm.
Fig. 2a shows the shockwave 30 propagating through the medium 28 (which could be the same material as in previous embodiments or a different material could be used), in the direction of the arrow, towards the gas pocket 22. Fig. 2b shows a later stage in the interaction, after the shockwave 30 has struck the gas pocket 22. The portion 27 of the shockwave 30 that has struck the edge of the pocket of gas 22 is reflected as a result of the large change in density from the medium 28 to the gas 22. This reflected portion 27 forms a rarefaction fan which propagates away from the gas pocket 22 and therefore creates a low pressure region between the reflected portion 27 and the gas pocket 22. The medium 28 flows into this low pressure region as a jet 29 which then traverses the gas pocket 22, trapping a fraction of the gas therein between the tip of the jet 29 and the tapering depression 24 in the surface 26, thereby causing compression and heating of the gas in the manner previously described.
Fig. 1 b shows a further configuration which is also suitable as an embodiment of this aspect of the invention.
Fig. 3 shows a further embodiment of the previous aspect of the invention in which a pocket of gas 32 is attached to a target surface 36 in a tapering depression 34. This embodiment is different from those previously described in that the pocket of gas 32 is separated from the medium 38 by a prefabricated membrane 33. The prefabricated membrane 33 is frangible i.e. it is designed to break on the impact of the shockwave 40. Once the prefabricated membrane 33 has been broken by the impact of the shockwave 40, the shockwave 40 continues to propagate into the depression 34 compressing the pocket of gas 32 in the same manner as for the previous embodiments.
Fig 4 is a variant of the embodiment shown in Fig. 2a. In this embodiment there are multiple smaller depressions 42 at the bottom on a large depression 44. The pocket of gas 46 is partially received both by the large depression 44 and by the multiple smaller depressions 42. In operation of this embodiment the jet formed when the shockwave (not shown) hits the pocket of gas 46 will highly compress multiple small volumes of the gas by trapping them in the small depressions 42, in a similar manner to that described above with reference to Figs. 2a and 2b.
Although specific examples have been given, it will be appreciated that there are a large number of parameters that influence the actual results achieved, for example liquid or gel medium density, ambient pressure and temperature, composition of the gas and of the liquid or gel, impact angle of the shockwave, target surface shape and micro-structure of the target surface.
In each of the embodiments described above, the diagrams shown are a vertical cross-section through a three-dimensional volume of gas and target surface and hence they depict embodiments that are rotationally symmetric. However, this is not essential to the invention. In particular the surface could comprise discrete surface portions in the rotational direction either instead of, or as well as in the vertical cross-section shown. In the latter case the target surface would be multifacetted. Each facet could give rise to separate but converging shockwaves.
In all of the embodiments described, the apparatus can be used by creating a shockwave in the medium which is incident upon a volume of gas containing deuterated water vapour.
In numerical modelling of the experiment, the techniques described herein give rise to a peak pressure of -20 GPa which is sufficient to cause temperatures inside the collapsed volume of gas in excess of 1x10⁶ Kelvin which can be sufficient for a nuclear fusion reaction of the deuterium atoms. In some non-limiting examples the resulting neutrons could be used in other processes, or could be absorbed by a neutron absorber for conversion of the kinetic energy of the neutrons to thermal energy and thus conventional thermodynamic energy generation.

Claims

A method of producing a localised concentration of energy comprising:
creating at least one shockwave (10; 30; 40) propagating through a non-gaseous medium (8; 28; 38) so as to be incident upon a pocket of gas (2; 22; 32; 46) within the medium (8; 28; 38) wherein the pocket of gas (2; 22; 32; 46) is attached to a surface (6; 26; 36) comprising a depression (4; 24; 34; 44) shaped so as to partially receive the gas pocket (2; 22; 32; 46), and

controlling the formation of a transverse jet (29) during collapse of the gas pocket (2; 22; 32; 46), wherein the depression (4; 24; 34; 44) in the surface (6; 26; 36) is designed to receive the transverse jet impact such that at least some of the gas in the pocket (2; 22; 32; 46) is trapped between the impacting jet (29) and the depression (4; 24; 34; 44) in the surface (6; 26; 36).
A method as claimed in claim 1, wherein the jet is arranged to strike an area of surface that has been prepared with a predetermined roughness (42) such that small portions of the pocket of gas (46) are trapped between the jet tip and the target surface.
A method as claimed in claim 1 or 2, wherein the depression (4; 24; 34; 44) in the surface (6; 26; 36) and gas pocket (2; 22; 32; 46) are arranged such that the initial contact region is a curve which forms a closed loop.
A method as claimed in claim 3, wherein a section of the depression (4; 24; 34; 44) in the surface (6; 26; 36) has a curvature greater than that of the tip of the jet (29) and wherein the section of the depression (4; 24; 34; 44) in the surface (6; 26; 36) is arranged such that the jet impacts therein.
A method as claimed in any preceding claims, wherein the depression (4; 24; 34; 44) in the surface (6; 26; 36) tapers in cross-section away from the mouth of the surface depression (4; 24; 34; 44).
A method as claimed in any preceding claim, wherein the depression (4) in the surface (6) has a depth greater than its width.
A method as claimed in any preceding claim, wherein the depression (4; 24; 34; 44) in the surface (6; 26; 36) comprises a plurality of discrete portions.
A method as claimed in claim 7, wherein the discrete portions are piecewise polynomial.
A method as claimed in any preceding claim, comprising using an explosive device to create the shockwave (10; 30; 40) with a pressure of between 0.1 GPa and 50 GPa.
A method as claimed in any of claims 1 to 8, comprising using lithotripsy device to create the shockwave (10; 30; 40) with a pressure of between 100 MPa and 1 GPa.
A method as claimed in any preceding claim, wherein the gas pocket (32) is formed with the use of a pre-manufactured membrane (33) that defines the boundary between the gas pocket (32) and the non-gaseous medium (38).
A method as claimed in claim 11, wherein the membrane (33) is frangible and is arranged to break upon impact from the shockwave (40).
A method as claimed in claim 11 or 12, wherein the prefabricated membrane (33) includes a line or region of weakness.
A method as claimed in any preceding claim employed to generate nuclear fusion reactions.
An apparatus for producing a localised concentration of energy comprising:
a non-gaseous medium having therein a pocket of gas (2; 22; 32; 46), wherein the pocket of gas is attached to a surface (6; 26; 36) comprising a depression (4; 24; 34; 44) shaped so as to partially receive the gas pocket (2; 22; 32; 46);

means for creating at least one shockwave (10; 30; 40) propagating through said medium so as to be incident upon said pocket of gas (2; 22; 32; 46); and

means to control the formation of a transverse jet (29) during collapse of the gas pocket (2; 22; 32; 46), wherein the depression (4; 24; 34; 44) in the surface (6; 26; 36) is designed to receive the transverse jet impact such that in use at least some of the gas in the pocket (2; 22; 32; 46) is trapped between the impacting jet (29) and the depression (4; 24; 34; 44) in the surface (6; 26; 36).